# N592US: 1988 Boeing 737-301, registration cancelled 2008-03-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 28, 2008 - Exported to: Tajikistan - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23937 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 2, 1988 - Certificate issued: February 19, 2008 - Last registry action: February 19, 2008 - Mode S code: A7A6A8 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N592US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=592US - Page: https://openairdocs.org/deregistered/N592US-2008-03-28 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SB07056](https://openairdocs.org/sdr/SB07056), Jul 15, 2007: WINDSHIELD. CRACKED. CHS - FLT - 1575 DURING CRUISE, EN ROUTE FROM DCA TO JAX, THE CAPTAIN'S NR 1 WINDSHIELD OUTER PANE CRACKED. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDUR - [SDR SB07051](https://openairdocs.org/sdr/SB07051), Jul 7, 2007: WIRE. BROKEN. MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 12, LT SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 12, LT SIDE. OPERATIONAL CHE - [SDR USAA061205](https://openairdocs.org/sdr/USAA061205), Oct 5, 2006: SKIN. CRACKED. FOUND CRACK BS 727D STRINGER 23L, DEFECT SIZE: 2". - [SDR USAA061206](https://openairdocs.org/sdr/USAA061206), Oct 5, 2006: SKIN. CRACKED. FOUND FUSELAGE SKIN CRACKED, BS 727D STINGER 23R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 98130, DEFECT SIZE: 2". - [SDR USAA061207](https://openairdocs.org/sdr/USAA061207), Oct 5, 2006: SKIN. CRACKED. FOUND SKIN CRACKED RADIO RACK EXHAUST CUTOUT. INSTALLED DOUBLER IAW EA 98129, DEFECT SIZE: 1". - [SDR USAA061201](https://openairdocs.org/sdr/USAA061201), Oct 4, 2006: FRAME. CORRODED. FOUND FRAME STA 380 BETWEEN STR 28R AND 28L. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 3, DEFECT SIZE: 2" BY 4". - [SDR USAA061202](https://openairdocs.org/sdr/USAA061202), Oct 4, 2006: SKIN. CRACKED. FOUND CRACK BS 727D STRINGER 23R. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER PER EA 98130, DEFECT SIZE: 2". - [SDR SB06095](https://openairdocs.org/sdr/SB06095), Oct 4, 2006: SWITCH. DIRTY. ON APPROACH, CREW REPORTED AN ASYMMETRICAL FLAP INDICATION AS THE TRAILING EDGE FLAPS LOCKED OUT. LT FLAP WAS INDICATING 15 UNITS AND THE RT FLAP 10 UNITS. PILO - [SDR SB06083](https://openairdocs.org/sdr/SB06083), Aug 28, 2006: TRANSMITTER. FAULTY. PHL - FLT238 - ON APPROACH TO PHL FROM DFW, CREW REPORTED THE FLAPS WOULD NOT MOVE FROM 10 UNITS TO 15 UNITS WHEN SELECTED. CREW EXECUTED A MISSED APPROACH, AND - [SDR SB06055](https://openairdocs.org/sdr/SB06055), May 30, 2006: TRANSMITTER. FAULTY. ORF - FLT32 - ON APPROACH TO ORF, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. FLIGHT LANDED WITHOUT INCIDENT AT 2 UNITS FLAP POSITION. MAINTENANCE CHECKED WIRING TO - [SDR SB06053](https://openairdocs.org/sdr/SB06053), May 20, 2006: LIGHT. CORRODED. FLL - MAINTENANCE REPORTED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BULBS AT LEFT EXTERIOR OVERWING EMERGENCY - [SDR SB06052](https://openairdocs.org/sdr/SB06052), May 19, 2006: INDICATOR. FAULTY. ON APPROACH TO PHL FROM ORD, AS CREW SELECTED FLAPS TO 10 UNITS FROM 5 UNITS, REPORTED THE RIGHT FLAP POSITION NEEDLE STOPPED AT 7 UNITS WHILE THE LEFT FLAP POS - [SDR SB06017](https://openairdocs.org/sdr/SB06017), Feb 15, 2006: BOTTLE. LOW. PIT - MAINTENANCE REPORTED THE MAIN ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE SHOWS NO GO. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRY DOOR ESCAPE SLIDE PER M - [SDR USAA051406](https://openairdocs.org/sdr/USAA051406), Nov 15, 2005: SKIN. PUNCTURED. RIGHT WING LEADING EDGE ABOVE NR 4 LEADING EDGE FLAP, APPROX L/E STA 205 DENTED. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER EA 9696 - [SDR USAA051405](https://openairdocs.org/sdr/USAA051405), Nov 15, 2005: SKIN. CRACKED. FWD SERVICE DOOR BOTTOM HINGE CUTOUT SKIN CRACKED. FABRICATED DOUBLER & FILLER PER SRM 52-00-01, 52-10-01. DEFECT SIZE: .250 INCH. - [SDR USAA051404](https://openairdocs.org/sdr/USAA051404), Nov 15, 2005: ANGLE. CRACKED. MAIN CABIN FLOOR BELOW FLOOR AT BS 616 LEFT SIDE CRACKED. REMOVED & REPLACED ANGLE, INSTALLED FILLER PER SRM 51-40-02 & TYP REP 53-62-01. DEFECT SIZE: .5 INCH. - [SDR USAA051403](https://openairdocs.org/sdr/USAA051403), Nov 15, 2005: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM TEE STA 986.5 RBL 20-30 CORRODED. REMOVED & REPLACED TEE PER TYP REP 53-60-01. DEFECT SIZE: 10 INCHES. - [SDR USAA051221](https://openairdocs.org/sdr/USAA051221), Oct 19, 2005: ANGLE. CORRODED. STA 907 TO 1006; NO TASK OF LEVEL, CORROSION. FABRICATED PART PER TR 549929, DWG 6941226, SRM 51-40-02, 53-60-15, DEFECT SIZE: 2L X 0.5W X .049 INCH DEEP. - [SDR USAA051220](https://openairdocs.org/sdr/USAA051220), Oct 19, 2005: SKIN. DEBONDED. FWD ENTRY DOOR INNER WALL AT LWR SKIN DISBONDED. FABRICATED REPAIR DOUBLER, FILLER PER TR 52-10-16, DEFECT SIZE: 0.250 INCH. - [SDR SB04161](https://openairdocs.org/sdr/SB04161), Dec 5, 2004: DUCT. DISCONNECTED. MCO FLT1222 EN ROUTE FROM PBI TO DCA, AT FL370, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW COULD NOT CONTROL CABIN ALTITUDE AND BOTH PACKS WERE ACTING ABNORM - [SDR USAA040407](https://openairdocs.org/sdr/USAA040407), Aug 6, 2004: SKIN. CRACKED. PIT - FOUND L/E SLAT CRACKED 3.5 INCHES, OUTBOARD, LOWER, TRAILING EDGE, NR 4 SLAT ASSEMBLY. INSTALLED DOUBLER PER SRM 57-43-01. (M) - [SDR USAA030214](https://openairdocs.org/sdr/USAA030214), Oct 17, 2003: STIFFENER. CORRODED. FOUND RADIAL STIFFENER CORRODED 2 INCH BY 1 INCH AREA, AFT PRESS BULKHEAD STATION 1016 AT BL 0. INSTALLED SPLICE SECTION AND REPAIR DOUBLERS PER EO 5302V112 AND - [SDR USAASB03142](https://openairdocs.org/sdr/USAASB03142), Aug 21, 2003: BEARING. WORN. UPON TOUCHDOWN AT ORF, FROM PHL, THE NR 2 MAIN LANDING GEAR TIRE BLEW. THE AIRCRAFT WAS OPERATING WITH MEL'S ON THE ANIT-SKID AND AUTO BRAKE SYSTEM. AIRCRAFT HA - [SDR USAASB03127](https://openairdocs.org/sdr/USAASB03127), Aug 3, 2003: CHARGER. INOPERATIVE. PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. AL - [SDR USAASB0301A](https://openairdocs.org/sdr/USAASB0301A), Jul 11, 2003: CHARGER. INOPERATIVE. PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER - [SDR USAASB03077](https://openairdocs.org/sdr/USAASB03077), Jun 10, 2003: LIGHT. INOPERATIVE. MAINTENANCE FOUND THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERAITONAL CHECK - [SDR USAASB02203](https://openairdocs.org/sdr/USAASB02203), Nov 4, 2002: LIGHT. INOPERATIVE. IND - MAINTENANCE FOUND THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ON THE FORWARD CLOSET INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT (ROUND - [SDR USAA011329](https://openairdocs.org/sdr/USAA011329), Oct 11, 2001: FLAP. DELAMINATED. PIT - FOUND INBOARD AFT FLAP DELAMINATED 15 INCHES BY 7 INCHES ROLLER AND 24 INCHES FROM INBOARD END, INBOARD AFT FLAP, BOTTOM SURFACES SKIN, INBOARD ROLLER SUP - [SDR USAASB01007](https://openairdocs.org/sdr/USAASB01007), Jan 15, 2001: PUMP. FAILED. PIT - FLT 9228 - DURING CRUISE, EN ROUTE FROM YUL-YYZ, THE NR 2 ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. DECISION WAS MADE FOR FLIGHT TO DIVERT TO PI - [SDR USAASB00155](https://openairdocs.org/sdr/USAASB00155), Jun 2, 2000: OUTFLOW VALVE. FAILED. PIT - FLT 1031 - FLIGHT WAS EN ROUTE FROM IAH TO PIT, WITH BOTH PACKS IN HIGHT FOR MAXIMUM COOLING. UPON REACHING FL370, CREW TURNED BOTH PACKS TO AUTO AND THE - [SDR USAASB99183](https://openairdocs.org/sdr/USAASB99183), Jul 24, 1999: CHARGER. FAILED. BDL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 20 INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AT STA 962L. OPE - [SDR USAASB99115](https://openairdocs.org/sdr/USAASB99115), Apr 29, 1999: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, FORWARD EXIT SIGNS IN FORWARD GALLEY, SEAT ROW 1 LOW LEVEL EVACUATION LIGHT, MAIN ENTRY DOOR - [SDR USAASB99082](https://openairdocs.org/sdr/USAASB99082), Mar 28, 1999: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE LOWER SIDEWALL EMERGENCY EXIT SIGNS FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA - [SDR USAASB98100](https://openairdocs.org/sdr/USAASB98100), Apr 18, 1998: CHARGER. FAILED. CLE - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE M1132 EMERGENCY LIGHT CHARGER ASSEMBLY. OPERATIONAL CHECK GO - [SDR USAA970297](https://openairdocs.org/sdr/USAA970297), Oct 10, 1997: FLOOR BEAM. CORROSION. CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES ON FLOOR BEAM STA 344 RBL 2 AND 10. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T- - [SDR USAA970296](https://openairdocs.org/sdr/USAA970296), Oct 10, 1997: FLOOR BEAM. CORROSION. CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES ON FLOOR BEAM STA 344 LBL 9.5, 21, 28, AND 49. CORROSION TASK NR C53-107-02. REMOVED AND - [SDR USAA970295](https://openairdocs.org/sdr/USAA970295), Oct 10, 1997: FLOOR BEAM. CORROSION. CLT - DURING Q-6 VISUAL INSPECTION, FOUND A CORRODED AREA OF 6 INCH BY 3 INCH STA 947 BL ZERO ON FLOOR BEAM. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER ON - [SDR USAASB96192](https://openairdocs.org/sdr/USAASB96192), Sep 13, 1996: DOOR. NOT CLOSED. CLT - FLT 1635 - AIRCRAFT DEVELOPED AN AIRFRAME VIBRATION AT LEVEL OFF AT FL 260. AFTER CHECKING THAT ALL AIRCRAFT SYSTEMS WERE NORMAL, THE CAPTAIN DECIDED TO D - [SDR USAASB95005](https://openairdocs.org/sdr/USAASB95005), Oct 28, 1995: OIL QTY XMITTER. FAILED. STL - FLT NR 0091 - EN ROUTE FROM PIT TO SAN, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE WAS FLUCTUATING BETWEEN 35 AND 40 PSI. FLIGHT CREW ACCOMPLI - [SDR USAA950544](https://openairdocs.org/sdr/USAA950544), May 29, 1995: CONTROL UNIT. FAILED. BWI - FLT 126 - FLIGHT EN ROUTE MCO TO DCA WHEN ANTI-SKID INOP LIGHT ILLUMINATED. FLIGHT DIVERTED TO BWI DUE TO RUNWAY LENGTH. MAINTENANCE REPLACED ANTI-SKID CO - [SDR USAA950448](https://openairdocs.org/sdr/USAA950448), Apr 29, 1995: CIRCUIT BREAKER. FAILED. PHL - FLT 941 - FLIGHT EN ROUTE BOS TO DCA, WHEN NR 1 ENGINE OIL TEMPERATURE AND PRESSURE INDICATORS DROPPED TO ZERO. CREW SHUT DOWN NR 1 ENGINE AND DIVERTED TO - [SDR USAA950382](https://openairdocs.org/sdr/USAA950382), Apr 18, 1995: CSD. FAILED. PIT - FLT 1669 - AFTER TAKEOFF FROM PHL EN ROUTE TO LAS, NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY NR 1 ENGINE GENERATOR DROPPING OFF LINE. CREW D ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19890130023189I](https://openairdocs.org/incident/19890130023189I), Jan 30, 1989: Boeing 737301 (N592US), San Jose, CA. Pressurization problems on takeoff. Returned. Found aft cargo door open. Warning light switch in closed position - [Incident 19881120063339I](https://openairdocs.org/incident/19881120063339I), Nov 20, 1988: Boeing 737301 (N592US), Las Vegas, NV. Passenger locked self in lavatory and became noisy. Emergency landing at Las Vegas. Escorted by police to hospital. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.